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    Unsteady Pressure Measurement on Oscillating Blade in Transonic Flow Using Fast-Response Pressure-Sensitive Paint 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 006:;page 61003
    Author(s): Watanabe, Toshinori; Azuma, Toshihiko; Uzawa, Seiji; Himeno, Takehiro; Inoue, Chihiro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A fast-response pressure-sensitive paint (PSP) technique was applied to the measurement of unsteady surface pressure of an oscillating cascade blade in a transonic flow. A linear cascade was used, and its central blade was ...
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    Effect of Shock Wave Behavior on Unsteady Aerodynamic Characteristics of Oscillating Transonic Compressor Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 144 ):;issue: 001:;page 11025-1
    Author(s): Gan, Jiuliang; Watanabe, Toshinori; Himeno, Takehiro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady behavior of the shock wave was studied in an oscillating transonic compressor cascade. The experimental measurement and corresponding numerical simulation were conducted on the cascade with different shock ...
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    Effect of Channel Size on Air-Cooling Performance in Interior Permanent Magnet Motor Driving Aviation Fans at High Altitude 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 145 ):;issue: 004:;page 41016-1
    Author(s): Ito, Yu; Watanabe, Toshinori; Seki, Naoki; Hirakawa, Karin; Inoue, Tomoya; Himeno, Takehiro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: To enhance worldwide environmental conditions, the air transport industry must drastically reduce carbon dioxide emissions. Electrification of aircraft propulsion systems is one way to meet this demand. In particular, the ...
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    Numerical Analysis of Flow in a Transonic Compressor With a Single Circumferential Casing Groove: Influence of Groove Location and Depth on Flow Instability 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 003:;page 31017
    Author(s): Sakuma, Yasunori; Watanabe, Toshinori; Himeno, Takehiro; Kato, Dai; Murooka, Takeshi; Shuto, Yukari
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of circumferential single grooved casing treatment on the stability enhancement of NASA Rotor 37 has been examined with computational fluid dynamics analysis. Stall inception mechanism of Rotor 37 is presented ...
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